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EN 14607-7:2004

Superseded

Superseded

A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.

View Superseded by

Space engineering - Mechnical - Part 7: Mechnical parts

Superseded date

01-04-2018

Superseded by

EN 16603-10:2018

Published date

04-08-2004

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Foreword
1 Scope
2 Normative references
3 Terms, definitions and abbreviated terms
  3.1 Terms and definitions
  3.2 Abbreviated terms
4 Requirements
  4.1 General
       4.1.1 Requirements overview
       4.1.2 Part classification
       4.1.3 Part types
       4.1.4 Application
  4.2 Mission
  4.3 Functionality
  4.4 Constraints
  4.5 Interface
  4.6 Design
  4.7 Verification
       4.7.1 Product assurance evaluation
       4.7.2 Part design verification and sizing
             requirements
       4.7.3 Part qualification
       4.7.4 Part acceptance
       4.7.5 Summary of the requirement levels
       4.7.6 Testing
  4.8 Production and manufacturing
  4.9 In-service
  4.10 Product assurance
  4.11 Deliverables
Annex A (informative) Example of a testing matrix
Bibliography

EN 14607 Part 7 of Space engineering - Mechanical defines the mechanical engineering requirements for mechanical parts.This document defines the requirements applicable to the selection, design, verification and application of mechanical parts to promote the use of high­quality non­critical mechanical parts that achieve robust functionality and satisfy the mission performance requirements.This document defines a pragmatic approach to the selection of parts by the mechanical and design engineer on the basis of their effect on the integrity of the equipment and to streamline the selection of space­proven rather than non space­proven parts during the design of a new equipment in order to select the least number of different parts to satisfy the mission requirements.It defines performance, design, test, product assurance and support activity requirements for the use of mechanical parts in space applications.When viewed from the perspective of a specific project context, the requirements defined in this document should be tailored to match the genuine requirements of a particular profile and circumstances of a project.NOTETailoring is a process by which individual requirements of specifications, standards and related documents are evaluated, and made applicable to a specific project by selection, and in some exceptional cases, modification of existing or addition of new requirements.

Committee
CEN/BT
DocumentType
Standard
PublisherName
Comite Europeen de Normalisation
Status
Superseded
SupersededBy

BS EN 14607-5-1:2004 Space engineering. Mechanical Liquid and electric propulsion for spacecraft
I.S. EN 14607-5-1:2004 SPACE ENGINEERING - MECHANICAL - PART 5-1: LIQUID AND ELECTRIC PROPULSION FOR SPACECRAFT
EN 14607-5-1:2004 Space engineering - Mechanical - Part 5-1: Liquid and electric propulsion for spacecraft

MIL-STD-1546 Revision B:1992 PARTS, MATERIALS, AND PROCESSES CONTROL PROGRAM FOR SPACE AND LAUNCH VEHICLES
MIL HDBK 5 : G_VOL2 METALLIC MATERIALS AND ELEMENTS FOR AEROSPACE VEHICLE STRUCTURES
EN 13291-1:1999 Space product assurance - General requirements - Part 1: Policy and principles
MIL-STD-410 Revision E:1991 NONDESTRUCTIVE TESTING PERSONNEL QUALIFICATION AND CERTIFICATION (EDDY CURRENT, LIQUID PENETRANT, MAGNETIC PARTICLE, RADIOGRAPHIC AND ULTRASONIC)
EN 13291-3:2003 Space product assurance - General requirements - Part 3: Materials, mechanical parts and processes
EN 13701:2001 Space systems - Glossary of terms
MIL-B-7883 Revision B:1968 BRAZING OF STEELS, COPPER, COPPER ALLOYS, NICKEL ALLOYS, ALUMINUM AND ALUMINUM ALLOYS
EN 13290-4:2001 Space project management - General requirements - Part 4: Project phasing and planning
EN 13291-2:2003 Space product assurance - General requirements - Part 2: Quality assurance
EN 14725:2003 Space engineering - Verification
EN 14607-2:2004 Space engineering - Mechanical - Part 2: Structural
EN 14607-8:2004 Space engineering - Mechanical - Part 8: Materials

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